FIELD: aeronautical engineering.
SUBSTANCE: proposed servo unit has body, electro-hydraulic power actuator, actuating cylinder, actuating cylinder piston rod travel limiter made in form of piston with bush, electro-hydraulic valve mounted in chamber, check valve, limiter control valve and connecting valves. Limiter chamber is located coaxially relative to actuating cylinder. Piston with limiter bush is mounted on actuating cylinder rod. Limiter chamber is connected with check valve and electro-hydraulic valve by means of passage through limiter control valve.
EFFECT: enhanced reliability.
1 dwg
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Authors
Dates
2006-06-27—Published
1978-07-31—Filed